Adjoint Based Aerodynamic Optimisation of a UCAV-Reference-Cited by-同舟云学术

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Adjoint Based Aerodynamic Optimisation of a UCAV

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Coppin Joe¹,Qin Ning¹

Affiliation:

1. University of Sheffield

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-146

Reference23 articles.

1. Bruce, R.J. "Low speed wind tunnel tests on the 1303 UCAV concept." QinetiQ, 2003, Technical Report, QINETIQ/FST/TR025502/1.0.

2. Bruce, R.J. "High speed wind tunnel tests on the 1303 UCAV concept." QinetiQ, 2003, Technical Report, QINETIQ/FST/TR030214/1.0.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Aerodynamic Shape Optimization of the Common Research Model Based on Improved SQP Algorithm;Lecture Notes in Electrical Engineering;2019

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